View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 62794U 26145.56283689 +.00000000 +00000-0 +15019-3 0 00005
2 62794 88.9720 86.0205 0012106 222.7029 137.3182 13.51011951 01
| Epoch (UTC): | 25 May 2026 13:30:29 |
| Eccentricity: | 0.0012106 |
| inclination: | 88.9720° |
| perigee height: | 1060 km |
| apogee height: | 1078 km |
| right ascension of ascending node: | 86.0205° |
| argument of perigee: | 222.7029° |
| revolutions per day: | 13.51011951 |
| mean anomaly at epoch: | 137.3182° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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